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Peaking Gas Turbine Capacity Enhancement Using Ice Storage for Compressor Inlet Air Cooling FREE

[+] Author Affiliations
Jerry A. Ebeling, Rick Halil

Burns & McDonnell Engineering Company, Kansas City, MO

Doug Bantam, Byron Bakenhus

Lincoln Electric System, Lincoln, NE

Henry Schreiber, Ron Wendland

Electric Power Research Institute, Palo Alto, CA

Paper No. 92-GT-265, pp. V004T10A011; 7 pages
doi:10.1115/92-GT-265
From:
  • ASME 1992 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 4: Heat Transfer; Electric Power; Industrial and Cogeneration
  • Cologne, Germany, June 1–4, 1992
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7896-5
  • Copyright © 1992 by ASME

abstract

Combustion turbine peaking units provide power for short time periods when hot, humid weather creates summer demand peaks. These same weather conditions degrade combustion turbine capacity and heat rate. Cooling combustion turbine inlet air increases its density and improves combustion turbine performance. A full size retrofit air chilling system for a G.E. MS7001B engine was installed by Lincoln Electric System, in Lincoln, Nebraska (U.S.A.), in an EPRI and American Public Power Associated supported and co-funded demonstration project. Detailed design and construction documents for the project were developed by Burns & McDonnell Engineering Company.

Copyright © 1992 by ASME
This article is only available in the PDF format.

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